Propeller Noise at Low Tip Speeds

Abstract

The study comprises an analytical and experimental investigation of the vortex noise generated by low-tip speed propellers. intially, the treatment of the subject is focussed on an examination of the origins of broadband noise and the methods by which these can be analytically represented. Subsequent noise measurements on simple-design propellers indicate how the typical spectra in the Strouhal frequency range are significantly influenced by an extensive range of high order harmonics of the blade passage frequency, and a treatment of this harmonic content is included in this study report. The broadband and harmonic components of noise data, obtained from propellers with blade number and blade angle variations, have been analyzed in detail and noise prediction methods have been derived for each. It is postulated that the noise source mechanisms may be associated with unstable laminar flow separation (or transition) at the blade surfaces. The report also includes a set of graphical procedures by which both harmonic and random spectral details of the radiated noise can be calculated by tip Mach numbers in the range 0.2 to 0.6.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1971
Accession Number
AD0731156

Entities

People

  • David F. Brown
  • John B. Ollerhead

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Sensors

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Bandwidth
  • Boundary Layer
  • Computational Fluid Dynamics
  • Flow Fields
  • Fluid Dynamics
  • Fluid Flow
  • Frequency Bands
  • Helicopter Rotors
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Propeller Noise
  • Test And Evaluation
  • Test Facilities
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Acoustics.
  • Aerodynamics.
  • Fluid Mechanics and Fluid Dynamics.